Design of X-and Ka-Band Reflectarray Antennas for Intercelestial Communication Using CubeSat Relay

Nishanth Virushabadoss, Nikita Mahjabeen, Harshpreet Singh Phull Bakshi, R. Henderson
{"title":"Design of X-and Ka-Band Reflectarray Antennas for Intercelestial Communication Using CubeSat Relay","authors":"Nishanth Virushabadoss, Nikita Mahjabeen, Harshpreet Singh Phull Bakshi, R. Henderson","doi":"10.1109/SHaRC51853.2021.9375885","DOIUrl":null,"url":null,"abstract":"This paper presents the design of reflectarray antennas operating at X- and Ka- bands with gains of 27 dBi and 34 dBi, respectively, which will be used for 3U CubeSat relay communication. The Lunar Reconnaissance Orbiter (LRO) collects around 573 GB of data per day and the data is sent to the ground station (WS1) located in White Sands, New Mexico [1]. The LRO communicates with the earth station an average of 4 times per day throughout the year [2]. The LRO has several instruments in the lunar orbit, ranging from passive imagers to an active altimeter, as well as a synthetic aperture radar [2]. There is a growing need to transfer more data to the earth station for future missions. In order to accomplish this goal, we propose to use a CubeSat relay between earth and the moon orbiter. This CubeSat will communicate with the deep space network (DSN) instead of communicating with WS1 and this will help in improving the connection time between the moon orbiter and ground station. The data rate of the proposed method would be 4.5 Mbps with binary phase shift keying (BPSK) modulation.","PeriodicalId":188904,"journal":{"name":"2021 IEEE Space Hardware and Radio Conference (SHaRC)","volume":"3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-01-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 IEEE Space Hardware and Radio Conference (SHaRC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SHaRC51853.2021.9375885","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 3

Abstract

This paper presents the design of reflectarray antennas operating at X- and Ka- bands with gains of 27 dBi and 34 dBi, respectively, which will be used for 3U CubeSat relay communication. The Lunar Reconnaissance Orbiter (LRO) collects around 573 GB of data per day and the data is sent to the ground station (WS1) located in White Sands, New Mexico [1]. The LRO communicates with the earth station an average of 4 times per day throughout the year [2]. The LRO has several instruments in the lunar orbit, ranging from passive imagers to an active altimeter, as well as a synthetic aperture radar [2]. There is a growing need to transfer more data to the earth station for future missions. In order to accomplish this goal, we propose to use a CubeSat relay between earth and the moon orbiter. This CubeSat will communicate with the deep space network (DSN) instead of communicating with WS1 and this will help in improving the connection time between the moon orbiter and ground station. The data rate of the proposed method would be 4.5 Mbps with binary phase shift keying (BPSK) modulation.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
基于立方体卫星中继的星际通信x波段和ka波段反射天线设计
设计了一种增益分别为27dbi和34dbi的X波段和Ka波段反射天线,用于3U立方体卫星中继通信。月球勘测轨道飞行器(LRO)每天收集大约573 GB的数据,这些数据被发送到位于新墨西哥州白沙的地面站(WS1)。LRO全年平均每天与地面站通信4次。LRO在月球轨道上有几个仪器,从被动成像仪到主动高度计,以及合成孔径雷达[2]。为了今后的任务,越来越需要向地面站传送更多的数据。为了实现这一目标,我们建议在地球和月球轨道器之间使用立方体卫星中继器。这颗立方体卫星将与深空网络(DSN)通信,而不是与WS1通信,这将有助于改善月球轨道器和地面站之间的连接时间。该方法采用二进制相移键控(BPSK)调制,数据速率为4.5 Mbps。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Wireless Payload Thermal-Vacuum Testing for Lunar Harsh Environment Design of X-and Ka-Band Reflectarray Antennas for Intercelestial Communication Using CubeSat Relay Efficient Data Uploads to Satellite Formations by Rateless Codes and Adaptive Tracking Extended Ground Station Concept and its Impact on the In-Orbit Communication with the Four-Nano-Satellite Formation NetSat Dual Mode Phased Array Antenna using Silicon RFICs based Integrated Beamforming Network
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1